Described herein are aerodynamically enhanced sensor housings. An aerodynamically enhanced sensor housing has an asymmetrical lateral cross-section that includes a first portion having a substantially spherical curvature and a second portion having a non-spherical curvature. The second portion having the non-spherical curvature may be elongated in relation to the first portion. An aerodynamically enhanced housing can also include one or more indentations formed in an exterior surface thereof to further enhance drag reducing characteristics of the housing. In addition, air flow characteristics around the sensor housing during vehicle operation can be assessed and a drag reduction protocol can be generated and implemented to further enhanced the drag reducing characteristics of the sensor housing.
Legal claims defining the scope of protection, as filed with the USPTO.
2. The computer-implemented method of claim 1, wherein the air flow characteristics comprise at least one of a level of air flow disruption of the impinging air on one or more portions of the exterior surface of the sensor housing or a direction of impingement of the impinging air.
3. The computer-implemented method of claim 2, wherein determining that the air flow characteristics fail to satisfy one or more drag reduction criteria comprises determining the level of air flow disruption is greater than a threshold level of permissible air flow disruption.
4. The computer-implemented method of claim 2, wherein determining that the air flow characteristics fail to satisfy one or more drag reduction criteria comprises determining that the direction of impingement of the impinging air exceeds a threshold angle.
5. The computer-implemented method of claim 1, wherein generating the drag reduction protocol comprises determining at least one of a modified rotational speed of the sensor housing or a modified relative positioning of the sensor housing with respect to a reference point on the vehicle to reduce the drag on the sensor housing.
6. The computer-implemented method of claim 1, wherein the sensor housing comprises an asymmetrical lateral cross-section, and wherein the asymmetrical lateral cross-section defines a first portion of the sensor housing having a substantially spherical curvature and a second portion of the sensor housing having a non-spherical curvature.
8. The system of claim 7, wherein the air flow characteristics comprise at least one of a level of air flow disruption of the impinging air on one or more portions of the exterior surface of the sensor housing or a direction of impingement of the impinging air.
9. The system of claim 8, wherein determining that the air flow characteristics fail to satisfy one or more drag reduction criteria comprises at least one of: determining the level of air flow disruption is greater than a threshold level of permissible air flow disruption or determining that the direction of impingement of the impinging air exceeds a threshold angle.
10. The system of claim 7, wherein generating the drag reduction protocol comprises determining at least one of a modified rotational speed of the sensor housing or a modified relative positioning of the sensor housing with respect to a reference point on the vehicle to reduce the drag on the sensor housing.
12. The sensor assembly apparatus of claim 11, wherein one or more indentations comprise a first indentation surrounded by two indentations each having a smaller depth, width, and radius of curvature compared to a depth, a width, and a radius of curvature of the first indentation.
14. The sensor assembly apparatus of claim 13, wherein a length of the elongated portion is inversely proportional to an amount of drag on the sensor housing.
15. The sensor assembly apparatus of claim 13, wherein the one or more indentations is a plurality of indentations that provides substantially complete coverage across the exterior surface of the sensor housing.
16. The sensor assembly apparatus of claim 13, wherein the one or more indentations comprise a first indentation and a second indentation, wherein at least one of a width or a depth of the first indentation is greater than a width or a depth of the second indentation.
17. The sensor assembly apparatus of claim 13, wherein the one or more indentations further comprise a first indentation, a second indentation, and a third indentation having substantially the same width and depth as the second indentation, and wherein the second indentation and the third indentation form a cluster around the first indentation.
18. The sensor assembly apparatus of claim 13, wherein the first portion of the sensor housing having the substantially spherical curvature is aligned with a direction of travel.
19. The sensor assembly apparatus of claim 13, wherein the air flow characteristics comprise at least one of a level of air flow disruption of the impinging air on one or more portions of the exterior surface of the sensor housing or a direction of impingement of the impinging air.
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March 18, 2020
July 4, 2023
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